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BF/Ops Flashcards

1
Q

Engine Fire During Ground Operations

A

THROTTLES - CUTOFF

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2
Q

Engine Fire During Flight

A

THROTTLE - IDLE

If engine fire switchlight remains illuminated, L or R FIRE DET FAIL illuminates, fire warning test fails, or fire conditions persist:

THROTTLE - CUTOFF
ENGINE FIRE SWITCH - PUSH
BOTTLE ARMED SWITCH - PUSH

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3
Q

Smoke Or Fumes In Aircraft

A

OXYGEN MASKS - DON / 100%

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4
Q

Pitch Trim/Roll Trim/Rudder Trim Runaway

A

TRIM INT & A/P DISENGAGE SWITCH - PUSH AND HOLD

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5
Q

Low Cabin Pressure

A

OXYGEN MASKS - DON / 100%

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6
Q

Takeoff - Time Limit (Minutes)

A

5 (1) Time limit starts when throttles first advanced for takeoff thrust.

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7
Q

Takeoff -
Maximum Observed ITT °C

A

700

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8
Q

Takeoff - N2 %

A

96

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9
Q

Takeoff - N1 %

A

104

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10
Q

Takeoff - Oil Pressure (2) PSI

A

60 to 83

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11
Q

Takeoff - Oil Temperature (° C)

A

10 to 121

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12
Q

Maximum Continuous - Time Limit (Minutes)

A

Continuous

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13
Q

Maximum Continuous - Maximum Observed ITT °C

A

680

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14
Q

Maximum Continuous -
N2 %

A

96

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15
Q

Maximum Continuous -
N1 %

A

104

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16
Q

Maximum Continuous - Oil Pressure (2) PSI

A

60 to 83

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17
Q

Maximum Continuous - Oil Temperature (°C)

A

10 to 121

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18
Q

Idle - Time Limit (Minutes)

A

Continuous

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19
Q

Idle - Maximum Observed ITT °C

A

580

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20
Q

Idle - N2 %

A

52 (Min)

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21
Q

Idle - Oil Pressure (2) PSI

A

40 (Min)

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22
Q

Idle - Oil Temperature (°C)

A

-40 to 121

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23
Q

Starting (4) - Maximum Observed ITT °C

A

550 - 600 4 SEC
600 - 700 2 SEC
700 - 720 1 SEC

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24
Q

Starting (4) - Oil Temperature (°C)

A

-40 (Min)

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25
Transient - **Maximum Observed ITT °C**
(720 2 SEC Max)
26
Transient - **N2 %**
96
27
Transient - **N1 %**
106
28
Transient - **Oil Pressure (2) PSI**
95 for 90 SEC
29
Transient - **Oil Temperature (°C)**
135 (Max) (15 MIN Max)
30
**Notes** (2) Normal Flight: Normal oil pressure is ____ to ____ PSI at N2 speeds above ____%. Oil pressure below ____ PSI is undesirable and should be tolerated only for safe recovery of the flight, preferably at reduced power setting. Oil pressure below ____ PSI is unsafe.
60 to 83 PSI 60% 60 PSI 40 PSI
31
**Notes** (3) Under cold starting conditions, oil pressure between ____ PSI and ____ PSI is limited to ____ seconds.
83 PSI and 95 PSI 90 seconds
32
**Notes** (4) The ITT during ground starts should normally not exceed ____ °C.
550° C
33
Normal hydraulic pressure ____ to ____ PSI
1350 to 1550 PSI
34
Normal nitrogen pressure ____ to ____ PSI
1350 to 1650 PSI
35
Normal oxygen pressure ____ to ____ PSI
1600 to 1850 PSI
36
Min battery voltage for battery start
22 volts
37
Max gen load prior to starting second engine
150 amps
38
Motoring of the starter is limited to: First, ___ seconds then ___ minutes cooling. Second, ___ seconds then ___ minutes cooling. Third, ___ seconds then ___ minutes cooling.
(1) 30 seconds, 5 minutes (2) 30 seconds, 15 minutes (3) 30 seconds, 60 minutes
39
Emergency Fuel / Minimum Fuel
300 lbs / 500 lbs
40
Maximum Fuel Imbalance - T.O./Touch & Go
100 lbs
41
Max Fuel Imbalance - Landing
300 lbs
42
Fuel crossfeed with 2 engine operating is limited to level flight with less than ___ lbs of fuel remains in the wing tank supplying fuel.
600 lbs
43
Max Ramp Weight
16,300 lbs
44
Max Takeoff Weight
16,100 lbs
45
Max Landing Weight
15,700 lbs
46
Extend flaps to 10 degrees
200 KIAS
47
Extend flaps > 10 degrees
170 KIAS
48
Flaps extended > 10 degrees
165 KIAS
49
Aircraft is limited to ____ KIAS or ____ MACH, whichever is less.
330 KIAS .78 MACH
50
Landing Gear/Lights
200 KIAS / FL 200
51
Wipers
200 KIAS
52
Tire
165 Knots GS
53
Max Tailwind
10 Knots
54
Max Crosswind (Dry)
25 Knots
55
Max Crosswind (Wet)
15 Knots
56
Max Crosswind (Icy)
10 Knots
57
Max Operating Altitude
FL 410
58
Yaw Damper required operable for flight above FL ____
FL 280
59
Do not use autopilot below ____ FT AGL
200 FT AGL
60
Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ___ ° C.
10° C
61
To ensure proper wing anti-ice operation, the throttles must be kept at ___% N2 minimum.
70% N2 minimum
62
Do not operate surface anti-ice systems in flight at ram air temperatures above ___ ° C.
10 ° C

T-1 (2 decks)

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